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GH4105
GH4105 is a Ni-Co-Cr base precipitation hardening deformation superalloy with a service temperature of 750 ℃~950 ℃. The alloy has high strength at room temperature and high temperature and good oxidation resistance, but its hot working performance and welding performance are general. It is suitable for manufacturing high-temperature components such as turbine blades, high-temperature bolts, etc. of aero-engine.
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product details
|
Brand |
GH4105 |
|
Similar brands |
GH105 |
|
Technicalstandard |
GB/T 14992-2005《Classification and designation of superalloy and intermetallic compound high-temperature materials》 HB/Z 140 《Heat treatment process of aviation superalloy》 |
| Classification |
Special alloy steel |
|
Performance |
Corrosion resistance |
|
Label |
Precipitation hardening nickel base alloy |
|
Explain |
GH4105 is a Ni-Co-Cr base precipitation hardening deformation superalloy with a service temperature of 750 ℃~950 ℃. The alloy has high strength at room temperature and high temperature and good oxidation resistance, but its hot working performance and welding performance are general. It is suitable for manufacturing high-temperature components such as turbine blades, high-temperature bolts, etc. of aero-engine. |
|
Density |
7.97g/cm3 |
Chemical composition:%
| Element |
Fe |
C |
Si |
Mn |
P |
S |
Cr |
Cu |
Mo |
TI |
Zr |
B |
Co |
Al |
|
Min. |
- |
0.12 |
- |
- |
- |
- |
14 |
- |
4.5 |
1.18 |
0.07 |
0.003 |
18 |
4.5 |
|
Max. |
1 |
0.17 |
0.25 |
0.4 |
0.015 |
0.01 |
15.7 |
0.2 |
5.5 |
1.5 |
0.15 |
0.01 |
22 |
4.9 |
Note: The above information is for reference only. Some elements in different standards and specifications may be different.
The information of the above materials is rough description, and any deviation may be used for reference only
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